EP0549098A1 - Unité de chargement renforcée pour avion - Google Patents

Unité de chargement renforcée pour avion Download PDF

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Publication number
EP0549098A1
EP0549098A1 EP92307929A EP92307929A EP0549098A1 EP 0549098 A1 EP0549098 A1 EP 0549098A1 EP 92307929 A EP92307929 A EP 92307929A EP 92307929 A EP92307929 A EP 92307929A EP 0549098 A1 EP0549098 A1 EP 0549098A1
Authority
EP
European Patent Office
Prior art keywords
container
door
slot
opening
bite
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP92307929A
Other languages
German (de)
English (en)
Inventor
Paul F. Mlakar
Joseph L. Smith
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JAYCOR
Original Assignee
JAYCOR
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by JAYCOR filed Critical JAYCOR
Publication of EP0549098A1 publication Critical patent/EP0549098A1/fr
Withdrawn legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D90/00—Component parts, details or accessories for large containers
    • B65D90/02—Wall construction
    • B65D90/029—Wound structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D88/00—Large containers
    • B65D88/005—Large containers of variable capacity, e.g. with movable or adjustable walls or wall parts, modular
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D88/00—Large containers
    • B65D88/02—Large containers rigid
    • B65D88/12—Large containers rigid specially adapted for transport
    • B65D88/14—Large containers rigid specially adapted for transport by air
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D90/00—Component parts, details or accessories for large containers
    • B65D90/008—Doors for containers, e.g. ISO-containers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D90/00—Component parts, details or accessories for large containers
    • B65D90/22—Safety features
    • B65D90/32—Arrangements for preventing, or minimising the effect of, excessive or insufficient pressure
    • B65D90/325—Arrangements for preventing, or minimising the effect of, excessive or insufficient pressure due to explosion, e.g. inside the container

Definitions

  • the present invention pertains to load carrying containers. More particularly, the present invention pertains to load carrying containers which will resist the blast effect of an explosive detonation inside the container.
  • the present invention is particularly, but not exclusively, useful as a container for carrying luggage and other cargo during transport by aircraft.
  • ULDs unit load devices
  • ULDs are shaped as boxes which can include appropriately sloped surfaces that conform the ULD to the aircraft's fuselage when the ULD is placed in the aircraft's cargo compartment.
  • the container is made of several panels which are joined together to form the ULD.
  • each ULD has a door or an access hatch which allows it to be opened for placing cargo in the ULD or for removing cargo from the ULD.
  • an object of the present invention to provide a hardened load carrying device for use in transporting cargo on aircraft which is able to resist internal blasts without rupturing. Another object of the present invention is to provide a hardened load carrying device which selectively incorporates reinforcing material at the points where an internal explosion generates the highest stress concentrations in the device. Yet another object of the present invention is to provide a hardened load carrying device which meets the regulatory standards for the use of such devices in air transport operations. Still another object of the present invention is to provide a hardened load carrying device which allows relative easy access into the device through an opening which can be effectively covered without compromising the efficacy of the device. Another object of the present invention is to provide a hardened load carrying device which is easy to use, relatively easy to manufacture, and comparatively cost effective.
  • a hardened load carrying device for holding luggage and cargo during air transport includes a container which is formed by a plurality of panels.
  • the panels are substantially flat and are formed with additional material at their peripheries.
  • they are joined together along their respective peripheries to form a box-like container of unitary construction which has reinforced joints.
  • the container is formed with an opening through which luggage and cargo can be placed in, or removed from, the container, and a slot borders at least part of the opening.
  • the slot itself is formed with a channel which has a pair of opposed and substantially parallel rims. Each of the rims has a lip which extends over part of the channel and each lip has a protrusion which projects part way into the channel. Together, these lips and their associated protrusions establish a pair of opposed crooked thumbs for the slot. As so positioned in the channel, a slit is created between the thumbs.
  • a door for covering the opening of the container, and for holding luggage or cargo in the container includes a bite which is formed along portions of the edge of door.
  • This bite includes a flange which is attached substantially perpendicular to the edge of the door panel and which projects therefrom in opposed directions. Further, the flange has a pair of extensions, each of which are on opposite sides of the door panel and which are oriented substantially parallel to the door panel. The extensions thus overlap the door panel to establish a pair of opposed crooked fingers.
  • the slot bordering the opening of the container is dimensioned to slidably receive the bite of the door.
  • the door can be engaged with the container to cover the opening and enclose the load in the container.
  • the slot grips the bite in response to an explosive blast within said container to resist rupturing of the device.
  • the hardened load carrying device is made of a blast resistive material, such as an epoxy or resin SPECTRA composite.
  • the container of the device is preferably of unitary construction and any additional strengthening material which may be needed is used selectively and only at points where relatively high stress concentrations are anticipated.
  • the crooked thumbs of the slot on the container and the crooked fingers of the bite on the door are replaced with other interlocking structures. Specifically, the protrusions from the lips in the slot which formed the crooked thumbs are eliminated.
  • the slot is substantially a T-shaped channel.
  • the flanges at the edge of the door remain, but the extensions from these flanges which formed the crooked fingers are eliminated. With this structure, the flanges are slidingly received in a cooperative T-shaped slot to interlock the door with the container.
  • the preferred embodiment and the alternate embodiment are substantially equivalent.
  • the door can be made to engage the container and through the center panel of the container (i.e. slide horizontally) rather than through the top or overhead panel (i.e. slide vertically).
  • HULD 10 hardened unit load device
  • HULD 10 includes a container 12 which is formed with an opening 14.
  • This HULD 10 has a box-like shaped container 12 that is made using a plurality of substantially flat panels.
  • the top panel 18, center panel 20, front panel 22, and sloped panel 24 are exemplary.
  • These, and the other panels which are necessary to create container 12, are connected to each other at joints 26 a,b,c etc. along their respective peripheries where the panels intersect each other.
  • front panel 22 is shown with two doors, the door 16 and a second door 28.
  • the material used for the construction of container 12, and the doors 16, 28, should exhibit a very high strength to weight ratio and offer high impact strength, thermal stability, chemical resistance and relatively low flammability and off-gas emissions.
  • a material is commercially available and is marketed under product names KEVLAR or SPECTRA.
  • the SPECTRA material used for HULD 10 is provided as a reinforced epoxy or resin SPECTRA laminate which can be molded to establish a container 12 having a unit body structure.
  • Preliminary estimates indicate that many layers (perhaps as many as twelve to twenty five layers, depending on the particular weave) of SPECTRA fabric may be required to withstand approximately one and a half (1.5) lb of TNT.
  • a HULD 10 capable of withstanding such a blast would have a tare weight of approximately one thousand (1,000) lb and the panels would be approximately thirty two one hundredths (0.32) inches thick.
  • Containers 12 having lower tare weights will, of course, be less tolerant to blasts.
  • Figure 2 shows that the edge 30 of door 28 includes a bite 32 which extends around the edge 30 of door 28.
  • the bottom edge 34 of door 28, however, is not formed with the bite 32.
  • an overlap 36 is formed along the bite 32 at the top of door 28, and the door 28 is provided with a device, such as the handle 38, which allows the door 28 to be manipulated.
  • the opening 14 is partially bordered by a slot 40 and a detent 42. The interaction between the edge 30 and bite 32 of door 16, or door 28, and the slot 40 and detent 42 which border the opening 14 will be best appreciated with reference to Figures 3 and 4.
  • the door 28 shown in Figure 3, and its interaction with the container 12, is representative of other similar structure disclosed for HULD 10 of the present invention.
  • Figure 3 shows that the bite 32 includes a flange 44 which is integrally attached to the edge 30 of door 28.
  • the flange 44 is oriented substantially perpendicular to the plane of the door panel 28 and extends in opposite directions from the edge 30.
  • Extensions 46 and 48 are integrally attached to the flange 44, as shown, and each extension 46,48 is oriented substantially parallel to the door panel 28.
  • the bite 32 is seen to include a pair of oppositely disposed crooked fingers 50a and 50b.
  • the crooked fingers 50a and 50b are identified in Figure 3 as being formed as part of the door panel 16.
  • the bite 32 on door 16 and the bite 32 of door 28 are substantially similar.
  • the slot 40 which borders an opening into the container 12 is formed to include a channel 52.
  • the channel 52 has a pair of opposed rims 54a and 54b, and also has a pair of lips 56a and 56b which respectively extend out and over the channel 52 from the rims 54a and 54b.
  • the protrusions 58a and 58b project part way into the channel 52, respectively from the lips 56a and 56b substantially as shown in Figure 3, to establish a pair of opposed crooked thumbs 60a and 60b for the slot 40.
  • a slit 62 is established between the thumbs 60a and 60b.
  • the bottom 34 of door 28 is not formed with a bite 32. Instead, the edge 30 is left exposed at the bottom 34 of door 28. Further, the bottom 64 of the opening which is covered by door 28 is not formed with a slot 40. Instead, the bottom 64 is formed with a detent 42. Accordingly, as shown in Figure 4, when door 28 is fully engaged with the container 12 to completely cover the opening, edge 30 at the bottom 34 of door 28 is inserted into the detent 42 at the bottom 64 of the opening. Additionally, when door 28 is fully engaged with the container 12, the overlap 36 rests against the outer surface of top panel 18.
  • the joints 26, which are established at the intersections of the panels that form container 12, are all reinforced in a manner similar to the structure shown in Figure 3 for individual joint 26e. This reinforcing is accomplished by providing additional material in the areas 66a and 66b that are adjacent to the bend in the joint 26e.
  • the thickness of the areas 66a and 66b around joint 26e is approximately twice the thickness of the remainder of the panels. This is done to satisfy structural stress analysis which indicate that the blast from an explosive which is detonated inside the container 12 will cause high stress concentrations around the joints 26. Additional strength can also be provided around the openings (e.g. opening 14) by establishing cross braces 68a, 68b, 68c and 68d, substantially as shown in Figures 3 and 4.
  • the joint 26 is not integral. Instead, and end plate 70 is used to join the abutting panels. As shown, the areas 66a and 66b again have a thickness which is approximately twice that for the rest of their respective panel and the endplate 70 has a thickness which is approximately equal to the thickness in the areas 66a and 66b.
  • fasteners well known in the pertinent art such as the rivets 72a and 72b, hold the endplate 70 against the areas 66 of the panels to establish the joints 26.
  • Figure 3 also indicates that the interior of container 12 can be covered with a crushable foam liner 74.
  • liner 74 is shown covering only a portion of the interior of the container 12, it is to be understood that the entire interior surface of container 12, as well as the inside surfaces of the doors 16 and 28, can be covered with the liner 74.
  • liner 74 can be made of any suitable material which will crush in response to an explosive blast and thereby absorb energy that would otherwise be directly imparted to the structural panels of the container 12. Additionally, if venting is provided for HULD 10, the crushable liner 74 will help mitigate the blast load which is felt by the interior of the container 12.
  • venting can be incorporated into the design of container 12 to appropriately reduce the effect of the blast.
  • the particular size and location of vents for the container 12 are a matter of design choice and can be varied according to the desires of the manufacturer. Regardless whether container 12 is vented, if it does not rupture from an internal explosion, the aggregate effect of a blast will be minimized both inside and outside the container 12 and, in most cases, the resultant damage can be effectively controlled.
  • the resin or epoxy SPECTRA composite material preferably used in the manufacture of the HULD 10 has superior strength characteristics.
  • SPECTRA is known to be an effective material for resisting puncture or rupture.
  • the use of a crushable liner 74 has some obvious advantages for reducing the impact of the blast.
  • the structural design of the HULD 10 for the interaction between the doors 16 and 28, and the container 12 causes these structures to cooperatively resist an internal blast.
  • FIG. 6 An alternate embodiment for the hardened unit load device of the present invention is shown in Figure 6 and is generally designated 100.
  • the device 100 includes a container 102 that is formed with an opening 104 through which articles, packages and luggage (not shown) can be placed in the container 102.
  • Figure 6 shows that the opening 104 of container 102 can be covered by a door 106.
  • the door 106 is engageable with the container 102 to slide over the opening 104 from the direction of the center panel 108 (i.e. slide horizontally), rather than from the direction of the top panel 110 (i.e. slide vertically).
  • the construction of the container 102 is substantially similar to the construction of the container 12.
  • the panel structure and the joint structure for the device 100 are the same as for the device 10.
  • the interlock between the door 106 and the container 102 is modified from what was previously disclosed for the engaging structure between the container 12 and the doors 16,28.
  • door 106 includes a panel 112 which is similar to the panels which are used in the manufacture of the container 12 or the container 102. Further, the panel 112 has an edge 114 and a flange 116 is attached along parts of the edge 114 substantially as shown. The flange 116 may, of course, be integral with the panel 112. As can be appreciated by reference to Figure 7, the combination of flange 116 and panel 112 forms a substantially T-shaped structure.
  • a handle 118 may be provided assist an operator in the engagement of the door 106 with the container 102.
  • a bottom panel 120 of the container 102 is formed with a T-shaped slot 122.
  • the slot 122 is a space which includes an open channel 124 and a slit 126.
  • the bottom panel 120 includes a pair of opposed rims 128 and 130 which extend substantially perpendicular from the plane of the panel 108.
  • a lip 132 and a lip 134 respectively extend from the lips 128 and 130 toward each other to form the T-shaped slot 122.
  • T-shaped slot 122 are such that they allow flange 116 to be slidingly received into the channel 124 of slot 122, and they allow the panel 112 of door 106 to pass through the slit 126 of slot 122.
  • Figure 8 also shows that top panel 110 of container 100 has a T-shaped slot 136 which is similar in structure to the slot 126.
  • the panel 112 of door 106 is formed with a flap 138.
  • the flap 138 extend behind front panel portion 140 (shown in Figure 6) when the door 106 is closed onto container 102. Also, it is to be appreciated that, when door 106 is closed, the surface 142 on that portion of flange 116 which is opposite flap 138 will abut against center panel 108.
  • panel 112 will resist an explosive blast within the container 102 through the interaction of flange 116 with slot 136 in top panel 110, the interaction of flange 116 with slot 122 in bottom panel 112, the abutment of flange 116 against center panel 108 and the abutment of flap 138 against front panel portion 140.
  • the door 106 can easily slide horizontally (i.e. perpendicularly to the center panel 108) to allow the operator access into the container 100. Once door 106 is closed the device 100 will resist the effect of an explosive blast within the container 102 through the various cooperations of structure described above.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Pressure Vessels And Lids Thereof (AREA)
  • Motor Or Generator Cooling System (AREA)
  • Connection Of Plates (AREA)
EP92307929A 1991-12-26 1992-09-01 Unité de chargement renforcée pour avion Withdrawn EP0549098A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US816309 1991-12-26
US07/816,309 US5312182A (en) 1991-12-26 1991-12-26 Hardened aircraft unit load device

Publications (1)

Publication Number Publication Date
EP0549098A1 true EP0549098A1 (fr) 1993-06-30

Family

ID=25220239

Family Applications (1)

Application Number Title Priority Date Filing Date
EP92307929A Withdrawn EP0549098A1 (fr) 1991-12-26 1992-09-01 Unité de chargement renforcée pour avion

Country Status (4)

Country Link
US (1) US5312182A (fr)
EP (1) EP0549098A1 (fr)
JP (1) JP2634360B2 (fr)
NO (1) NO177930C (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0663350A1 (fr) * 1994-01-12 1995-07-19 Jaycor Unité de chargement téléscopique pour avion
EP0671343A1 (fr) * 1994-03-09 1995-09-13 Jaycor, Inc. Unité de chargement renforcée pour avion
FR2726255A1 (fr) * 1994-10-26 1996-05-03 Pigeaud Philippe Conteneur frigorifique et autonome pour le transport aerien de denrees perissables
US8960468B2 (en) 2007-09-20 2015-02-24 Norduyn Inc. Collapsible container
WO2019097042A1 (fr) * 2017-11-20 2019-05-23 Heinz Buse Conteneur interchangeable destiné au transport de marchandises et système de conteneur interchangeable

Families Citing this family (19)

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Publication number Priority date Publication date Assignee Title
US6341708B1 (en) 1995-09-25 2002-01-29 Alliedsignal Inc. Blast resistant and blast directing assemblies
US6991124B1 (en) 1995-09-25 2006-01-31 Alliedsignal Inc. Blast resistant and blast directing containers and methods of making
US7185778B1 (en) 1995-09-25 2007-03-06 Allied-Signal Inc. Barrier units and articles made therefrom
US6237793B1 (en) 1998-09-25 2001-05-29 Century Aero Products International, Inc. Explosion resistant aircraft cargo container
US6322179B1 (en) * 1999-08-05 2001-11-27 Kurt D. Hillemann Orientation adjustable insulated workpiece for welding
TW543630U (en) * 2002-05-27 2003-07-21 Ind Tech Res Inst Connection device for use with a blast-proof container
US6988781B2 (en) 2002-12-27 2006-01-24 Jaycor Airtight blast resistant cargo container
US20070039954A1 (en) * 2003-05-23 2007-02-22 Industrial Technology Research Institute Connection device for use with a blast-resistant container
US7343843B2 (en) * 2003-07-31 2008-03-18 Blast Gard International Explosive effect mitigated containers and enclosing devices
US8316752B2 (en) * 2003-07-31 2012-11-27 Blastgard Technologies, Inc. Acoustic shock wave attenuating assembly
CN102414012A (zh) 2009-04-23 2012-04-11 帝斯曼知识产权资产管理有限公司 压缩板材
US8784605B2 (en) 2010-06-02 2014-07-22 International Composites Technologies, Inc. Process for making lightweight laminated panel material for construction of cargo containers
EP2492217B1 (fr) 2011-02-22 2013-11-20 Sächsisches Textilforschungsinstitut e.V. Système de conteneurs de chargement résistant contre le souffle, léger et entièrement à base de textile et son procédé de fabrication
US8800797B2 (en) 2012-07-05 2014-08-12 Richard L. Fingerhut Heat and explosion resistant cargo container
EP2950036B1 (fr) * 2014-05-28 2017-12-13 Dynasafe Protection Systems AB Récipient résistant aux explosions
DE102015113449B4 (de) * 2015-08-14 2024-02-01 Airbus Operations Gmbh Befüllbarer Lagercontainer zur Unterbringung in einem Frachtraum eines Luftfahrzeugs
CN106628590A (zh) * 2016-11-25 2017-05-10 吴保康 一种稳定型配电柜运输用放置架
CN110371498B (zh) * 2019-05-31 2020-08-11 中车齐齐哈尔车辆有限公司 滑动门组件及具有其的集装箱
US11919707B2 (en) * 2019-06-27 2024-03-05 Bradford Company Sliding cover assembly for a dunnage container

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5599082A (en) * 1991-12-26 1997-02-04 Jaycor Hardened aircraft unit load device
EP0663350A1 (fr) * 1994-01-12 1995-07-19 Jaycor Unité de chargement téléscopique pour avion
EP0671343A1 (fr) * 1994-03-09 1995-09-13 Jaycor, Inc. Unité de chargement renforcée pour avion
FR2726255A1 (fr) * 1994-10-26 1996-05-03 Pigeaud Philippe Conteneur frigorifique et autonome pour le transport aerien de denrees perissables
US8960468B2 (en) 2007-09-20 2015-02-24 Norduyn Inc. Collapsible container
WO2019097042A1 (fr) * 2017-11-20 2019-05-23 Heinz Buse Conteneur interchangeable destiné au transport de marchandises et système de conteneur interchangeable

Also Published As

Publication number Publication date
NO923394L (no) 1993-06-28
JP2634360B2 (ja) 1997-07-23
JPH06239385A (ja) 1994-08-30
NO177930B (no) 1995-09-11
NO177930C (no) 1995-12-20
NO923394D0 (no) 1992-08-31
US5312182A (en) 1994-05-17

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